EP0559171A2

EP0559171A2 - Vehicular suspension system

Info

Publication number: EP0559171A2
Application number: EP93103389A
Authority: EP
Inventors: Mitsuo C/O Unisia Jecs Corporation Sasaki
Original assignee: Unisia Jecs Corp
Current assignee: Hitachi Unisia Automotive Ltd
Priority date: 1992-03-03
Filing date: 1993-03-03
Publication date: 1993-09-08
Anticipated expiration: 2013-03-03
Also published as: JPH05238224A; DE69311399D1; US5430648A; DE69311399T2; EP0559171A3; EP0559171B1

Abstract

A vehicular suspension system comprises a hydraulic damper including a valve element (34) having a plurality of positions and a pulse motor (152) drivingly coupled with the valve element (34). A control unit (154) is operatively coupled with the pulse motorr (152). In order to avoid occurrence of loss of synchronism of the pulse motor (152), the pulse motor (152) is held stationary for a predetermined period of time (a settling time) after it has been determined that the pulse motor (152) must invert its direction of motion to reach a target position (TARGET).

Description

BCKGROUND OF THE INVENTION

The present invention relates to a vehicular suspension system and a method of controlling a vehicular suspension system.
A vehicular suspension system is known which comprises a plurality of shocjk absorbers, each including a hydraulic damper. The hydraulic damper includes a valve element having a plurality of positions and an actuator in the form of a pulse or stepper motor drivingly coupled with the valve element. A control unit is operatively coupled with each of the pulse motors. Each of the pulse motors is subject to the control unit such that if a target position is subject to a change, the pulse motor turns concurrently with the occurence of this change to approach or reach the new target position. Since turning of the pulse motor and the subsequent turning of the valve element is resisted by flow of hydraulic fluid passing through the hydraulic damper, occurrence of vibration is unavoidable. However, there occurs circumastance where resonance is induced by vibration. If the resonace inducing vibration takes place, it is difficult to find the appripriate timing to drive the pulse motor. Thus, the loss of synchronism of the pulse motor is unavoidable in the known system.
Accordingly, an object of the present invention is to improve a vehicular suspension system such that the actuator for the valve element of the adjustable hydraulic damper moves smoothly by avoiding the occurrence of loss of synchronism of the actuator.

SUMMARY OF THE INVENTION

According to one aspect of the present invention, there is provided a vehicular suspension system comprising:
a hydraulic damper including a valve element having a plurality of positions and an actuator drivingly coupled with the valve element; and
a control unit operatively coupled with the actuator,
wherein the actuator is held stationary for a predetermined period of time after it has been determined that the actuator must invert its direction of motion to reach a target position.
According to another aspect of the present invention, there is provided a method of controlling a vehicular suspension system comprising:
a hydraulic damper including a valve element having a plurality of positions and an actuator drivingly coupled with the valve element; and
a control unit operatively coupled with the actuator,
wherein the actuator is held stationary for a predetermined period of time after it has been determined that the actuator must invert its direction of motion to reach a target position.

BRIEF DESCRIPTION OF THE DRAWINGS

Fig. 1 is a schematic representation of a vehicular suspension system installed in an automobile;
Fig. 2 is a control block diagram;
Fig. 3 is an illustration of a shock absorber partly sectioned;
Fig. 4 is a fragmentary diagrammatic view of a hydraulic damper of the shock absorber shown in Fig. 3, this view resulting from combining different sections taken through the line IV-IV of Figs. 5, 6 and 16;
Fig. 5 is a section taken through the line V-V of Fig. 4;
Fig. 6 is a section taken through the line VI-VI of Fig. 4;
Fig. 7 is a diagrammatic section taken through the line VII-VII of Fig. 4, showing a control rod assembly in a first angularly displaced position;
Fig. 8 is a diagrammatic section taken through the line VIII-VIII of Fig. 4, showing the control rod assembly in the first angularly displaced position;
Fig. 9 is a diagrammatic section taken through the line IX-IX of Fig. 4, showing the control rod assembly in the first angularly displaced position;
Figs. 10, 11 and 12 are similar views to Figs. 7, 8 and 9, but showing the control rod assembly in a neutral position;
Figs. 13, 14 and 15 are similar views to Figs. 7, 8 and 9, but showing the control rod assembly in a second angularly displaced position;
Fig. 16 is a section taken through the line XIII-XIII of Fig. 4;
Fig. 17 is an exploded view of a portion of the control rod assembly;
Fig. 18 is a diagrammatic graphical representation of the variation of damping force versus angular displacement of the control rod assembly with the same piston speed together with a bar graph, at the bottom, showing opening ranges of respective passage ways in relation to angular position of the control rod assembly;
Fig. 19 shows various damping force versus piston speed characteristics of the hydraulic damper;
Fig. 20 shows damping force versus piston speed characteristic curves at the first angularly displaced position through counterclockwise rotation of the actuator from the neutral position;
Fig. 21 shows damping force versus piston speed characteristic curves at the neutral position;
Fig. 22 shows damping force versus piston speed characteristic curves at the second angularly displaced position through clockwise rotation of the actuator from the neutral position;
Fig. 23 is a flow diagram of a actuator drive routine; and
Figs. 24A, 24B, 24C and 24D show a time sequence chart showing a vertical relative speed indicative signal in Fig. 24A, a target position indicative signal (TARGET in Fig. 23) in Fig. 24B, a present position indicative signal (OUTPUT in Fig. 23), and an actuator position indicative signal in Fig. 24D.

DETAILED DESCRIPTION OF THE INVENTION

Referring to Fig. 1, there are illustrated four shock absorbers SA installed in a conventional manner between a vehicle body and the corresponding axles carrying tyres. Illustrated adjacent the shock absorbers SA are G sensors 150 which detects vertical acceleration of the vehicle body at portions adjacent the shork absorbers SA, respectively. Sensor outputs of the G sensors 150 are fed to a control unit 154 mounted within a passenger compartment of the vehicle. Mounted on the shock absorbers are actuators 152 which are subject to the control unit 154. Each of the actuators 152 is in the form of a pulse or stepper motor.
Referring to Fig. 2, the control unit 154 is operatively coupled with the G sensors 150. Specifically, the control unit 154 includes an interface circuit 156, a central processing unit (CPU) 158, and a drive circuit 130. Via the interface circuit 156, the sensor outputs of the G sensors 150 are read at regular intervals and the read data are processed via integration to give vertical speeds. Based on the speeds, target positions which the pulse motors 152 should assume are determined. Then, direction of motion in which each of the pulse motor 152 should rotate to assume the target position assigned thereto is determined. The CPU 158 gives instructions to the drive circuit 160. Based on the instructions, the drive circuit 160 controls the pulse motors 152.
Referring to Fig. 3, each shock absorber SA comprises a cylinder 10, a piston 18 defining one one side an upper chamber 20 and on the opposite side a lower chamber 22 within the cylinder 10, an outer casing 162 Surrounding the cylinder 10 to define therearounda reservoir 164, a base 166 partly defining the lower chamber 22, a rod guide 168 slidably guiding a rod 12, a suspension spring 170 and a stop rubber 172.
Fig. 4 illustrates in section an adjustable hydraulic damper which forms a part of the shock absorber SA shown in Fig.3.
Referring to Fig. 4, the adjustable hydraulic damper generally comprises the cylinder 10, a piston rod assembly including the piston rod 12 hollowed, a hollow rebound stopper 14 threadedly secured on the end of the piston rod 12 and a hollow rod 16 threadedly secured on the rebound stopper 14, and a damping piston assembly secured on the hollow rod 16. The piston assembly includes a piston 18. The piston 18 divides the interior of the cylinder 10 into upper and lower chambers 20 and 22 containing hydraulic damping fluid. The piston 18 is fitted with an extension phase damping valve 24, a contraction phase damping valve 26, an extension phase one-way valve 28 and a contraction phase one-way valve 30. A control rod assembly includes a rod 32 and a hollow control rod 34 secured on the end of the rod 32. The rod 32 is rotatably mounted within the hollow interior of the piston rod 12 and has its lower end portion rotatably supported by a bushing 36 disposed between the rebound stopper 14 and the hollow rod 16. As seen in Fig. 3, the upper end of the rod 32 is drivingly coupled with the pulse motor 152. The hollow control rod 34 which serves as a valve element is rotatably mounted within the cylindrical bore of the hollow rod 16. The lower end of the hollow control rod 34 has a bushing 38.
The piston 18 has four pairs of extension phase bores 40 and the extension phase damping valve 24 for damping in the extension phase, the valve being in the form of a stack of disc springs. As best seen in Figs. 5 and 6, each of the four pairs of extension phase bores 40 have upper ends opening to one of four radial passages 42 which are provided in the upper axial end of the piston 18 and adjacent the contraction phase damping valve 26. The lower ends of each of the four pairs of extension phase bores 40 open to one of four equi-angularly distant recesses 44 which are provided in the lower axial end of the piston 18 and adjacent the extension phase damping valve 24. An annular recess 44 is provided in the lower axial end of the piston 18 and adjacent the extension phase damping valve 24 in such a manner as to surround the four equi-angularly distant recesses 44. The four equi-angularly distant recesses 44 communicate with the upper chamber 20 through the extension phase bores 40 and the radial passages 42. The annular recess 46 communicates with the upper chamber 20 through radial recesses 48, an annular passage 50, discharge bores 52, axial passages 54 formed between the cylindrical interior of the hollow rod 16 and grooves 56, inlet bores 58, an annular passage 60 and the radial passages 42. A valve body 64 for the extension phase one-way valve 28 is secured on the hollow rod 16. In the lower axial end of this valve body 64, radial recesses 66 are provided adjacent the extension phase one-way valve 28. These radial recesses 66 communicate with the upper chamber 20 through discharge bores 68, the axial passages 54, the inlet bores 58, the annular passage 60 and the radial passages 42. The hollow control rod 34 has a central bore 70 opening to the lower chamber 22. The central bore 70 communicates with the upper chamber 20 through axial slots 72, bypass bores 74, the annular passage 60 and the radial passages 42.
For extension phase, there are four passage ways open when the hollow control rod 34 assumes the neutral position as shown in Figs. 5, 6, 10, 11 and 12. Namely, these four passage ways are;
A first extension phase passage way D which allows a flow of damping fluid through the extension phase bores 40 to the four equi-angularly distant recesses 44 and into the lower chamber 22 deflecting open the extension phase damping valve 24;
A second extension phase passage way E which allows a flow of damping fluid to the annular recess 46 through the inlet bores 58, the axial passages 54 and the discharge bores 52 and into the lower chamber 22 deflecting open the extension phase damping valve 24;
A third extension phase one-way passage way F which allows a flow of damping fluid to the radial recesses 66 through the inlet bores 58, the axial passages 54 and the, discharge bores 68 and into the lower chamber 22 deflecting open the one-way valve 28; and
A fourth or bypass passage way G which allows a flow of damping fluid into the lower chamber 22 through the bypass bores 74, the axial slots 72 and the central bores 70.
For the contraction phase, the piston 18 has four contraction phase bores 76 and the contraction phase damping valve 26 is also in the form of a stack of disc springs. As best seen in Fig. 2, each of the four contraction phase bores 76 has an upper end opening to one of four equi-angularly distant recesses 78 which are provided in the upper axial end of the piston and adjacent the contraction phase damping valve 26. The contraction phase bores 76 have lower ends communicating with a circumferential inlet groove 80 opening to the lower chamber 22. A valve body 82 for the contraction phase one-way valve 30 is secured on the hollow rod 16. In the lower axial end of this valve body 82, an annular recess 84 is provided adjacent the contraction phase one-way valve 30. This annular recess 84 communicates with the lower chamber 22 through transverse bores 86, discharge bores 88 and the central bore 70.
For the contraction phase, there are three passage ways open When the hollow control rod 34 assumes the neutral position as shown in Figs. 5, 6, 10, 11 and 12. Namely, the three passage ways are;
A first contraction phase passage way H which allows a flow of damping fluid through the contraction phase bores 78 to the equi-angularly distant recesses 78 and into the upper chamber 20 deflecting open the contraction phase damping valve 26;
A second contraction phase one-way passage way J which allows a flow of damping fluid through the central bore 70, the discharge bores 88, the transverse bores 86 to the annular recess 84 and into the upper chamber 20 deflecting open the contraction phase one-way valve 30; and
The before-mentioned bypass passage way G.
If, with a soft contraction phase maintained, a hard extension phase is desired, the hollow control rod 34 is rotated counterclockwise from the neutral position as shown in Figs. 10 to 12 to a first angularly displaced position as shown in Figs. 7 to 9. In this first angularly displaced position, the bypass passage way G and the extension phase passage ways E and F are closed although the contraction phase passage way J remains_, open. At the left-hand half of Fig. 18, there is shown variation of a damping force DF(E) for extension phase and a damping force DF(C) for contraction phase in relation to various angular positions from the neutral position to the first angularly displaced position. Since the contraction phase passage way J is left open, the damping force DF(C) for contraction phase is kept low. As shown in Fig. 18, the damping force DF(E) for extension phase gradually increases owing to this counterclockwise motion from the neutral position toward the first angularly displaced position.
If, with a soft extension phase maintained, a hard contraction phase is desired, the hollow control rod 34 is rotated clockwise from the neutral position as shown in Figs. 10 to 12 to a second angularly displaced position as shown in Figs. 13 to 15. In this second angularly displaced position, the bypass passage way G and the contraction phase passage way J are closed although the extension phase passage way E and F remain open. At the right-hand half of Fig. 18, there is shown variation of the damping force DF(E) for extension phase and the damping force DF(C) for contraction phase in relation to various angular positions from the neutral position to the second angularly displaced position. Since the extension phase passage ways E and F are left open, the damping force DF(E) for extension phase is kept low. As shown in Fig. 18, the damping force DF(C) for contraction phase gradually increases owing to this clockwise motion from the neutral position to the second angularly displaced position.
Referring to Figs. 4, 16 and 17, the hollow control rod 34 has an upper end portion formed with two cutouts 90 to provide a diametrical land 92 with two parallel walls. The diametrical land 92 is recived in a key opening 94 of a positioning plate 96. The positioning plate 96 has two diametrically opposed projections 98 received in the corresponding two grooves 100 of an upper stud portion 102 of the hollow rod 16. The positioning plate 96 has inwardly projecting stoppers 104 which abut the diametrical land 92 to limit angular motion of the hollow control rod 34. The positioning plate 96 is interposed between the bushing 36 and the stud portion 102 of the hollow control rod 16. For smooth motion and axial positioning of the hollow control rod 34 within the cylindrical interior of the hollow rod 16, two kinds thrust washers 106 and 108 are disposed between the bushing 36 and the top end of the diametrical land 92 and the bushing 38 supports the lower end of the hollow control rod 34. The use of the positioning plate 96 and the diametrical land 92 assures easy positioning of the hollow control rod 34 without exterting any bending stress on the hollow control rod 34.
In assembly, after mounting the control rod assembly 32, 34 within the piston rod assembly 12, 14, 16, the piston assembly is mounted in the following manner. The valve body 82, the contraction phase one-way valve 30, a washer 110, a collar 112, a washer 114, the contraction phase damping valve 26, the piston 18, the extension phase 24, a washer 116, the valve body 64, the extension phase one-way valve 28, a washer 118 and a collar 120 are mounted around the hollow rod 16 and fixedly secured thereon by tightening a nut 122.
As shown in Fig. 19, the adjustable hydraulic damper can provide a number of different damping force versus piston speed characteristics corresponding depending upon different angularly displaced positions of the valve element or the hollow control rod 34 (see Fig. 4).
Fig. 20 shows damping force versus piston speed characteristic curves at the first angularly displaced position through counterclockwise rotation of the pulse motor 152 from the neutral position.
Fig. 21 shows damping force versus piston speed characteristic curves at the neutral position.
Fig. 22 shows damping force versus piston speed characteristic curves at the second angularly displaced position through clockwise rotation of the pulse motor 152 from the neutral position.
Referring to Figs. 2, 24A and 24B, the control unit 154 is further explained. In the control unit 154, the vertical speed is derived from the sensor output of the G sensor 150 via integration process. Fig. 24A shows one example of variation a signal V indicative of the vertical speed with respect to time. There is determined a target position which the pulse motor 152 should take for the shock absorber SA to exibit the most appropriate damping characteristic to the instant value of the vertical speed indicative signal. Fig. 24B shows the variation of a signal TARGET indicative of the determined target position with respect to time. The manner of determining the target position is such that when the vertical speed indicative signal V indicates that the instant speed is directed upward, with the extension phase damping characteristic set hard, the damping characteristic for the extension phase is varied stepwisely in accordance with the magnitude of the vertical speed signal V, while when the instant vertical speed, indicative signal V indicates that the instant speed is directed downward, with the contraction phase damping characteristic set hard, the damping characteristic for the contraction phase is varied stepwisely in accordance with the magnitude of the vertical speed indicative signal V. The determined target position (TARGET) is compared with a present position (OUTPUT). In response to result of this comparison, it is determined which direction the pulse motor 152 should turn. Specifically, it is determined whether the pulse motor 152 should turn clockwise (step-up) or counterclockwise (step-down) until the present position (OUTPUT) becomes equal to the target position (TARGET). Fig. 24C shows how the present position OUTPUT varies with respect to time. Fig. 24D shows how actual position of the pulse motor 152 varies with respect to time.
Referring to Fig. 23, an actuator drive routine is explained. Execution of this routine is repeated and initiated upon elapse of one-cycle time of 0.1 msec.
In Fig. 23, at a step 201, there is an interrogation whether a flag SETTLING is set or not. If this is the case (YES), the flow proceeds to a step 202. If the result of this interrogation results in negative (NO), the flow proceeds to a step 205. At the step 202, an increment of a counter SET CNT is carried, out, viz., the counter SET_CNT is increased by one (1). Then, the flow proceeds to a step 203 where there is an interrogation whether the content of the counter SET_CNT is greater than or equal to five (5) or not. If this is the case (YES), the flow proceeds _, to a step 204. If the interrogation at the step 203 results in negative (NO), the the flow comes to an end. At the step 204, the SETTLING flag is cleared. After this step 204, the flow comes to an end.
If the interrogation at the step 201 results in negative (NO), the flow proceeds to the step 205. At the step 205, there is an interrogation whether the present position OUTPUT is equal to the target position TARGET or not. If this is the case (YES), the flow proceeds, to a step 206. If the interrogation at the step 205 results in negative (NO), the flow proceeds to a step 208. At the step 206, there is an interrogation whether the content of the counter SET_CNT is greater than or equal to five (5) or not. If this is the case (YES), the flow come to an end. If the interrogation at the step 206 results in negative (NO), the flow proceeds to a step 207. At the step 207, the content of the counter SET CNT is cleared and then the flow comes toan end.
If the interrogation at the step 205 results in negative (NO), there is an interrogation at the step 208 whether the present position OUTPUT is smaller than the target position TARGET. If this is the case (YES), viz., in the case where the pulse motor 152 should turn clockwise (step-up) to reach the target position TARGET, the flow proceeds to a step 209. If the interrogation at the step 208 results in nagative, viz., in the case where the the pulse motor 152 should turn counterclockwise (step-down) to reach the target position TARGET, the flow proceeds to a step 210.
At the step 209, there is an interrogation whether the content of the counter SET_CNT is greater than or equal to five (5) or not. If this is the case (YES), the flow proceeds to a step 212. If the interrogation at the step 209 results in nagative, the flow proceeds to a step 211.
There is a flag CW/CCW (clockwise or counterclockwise) which switches to a CW position or a CCW position. The position of the CW/CCW flag is indicative of the direction in which the pulse motor 3 turned previously. The CW position corresponds to previous clockwise rotation of the pulse motor 152, while the CCW position corresponds to previous counterclockwise rotation, At the step 211, there is an interrogation whether the CW/CCW flag takes CW position Or CCW position. If the interrogation at the step 211 indicates that CW/CCW flag takes the CW position, the flow proceeds to a step 212, while if it indicates that CW/CCW flag takes the CCW position, the flow proceeds to a step 207.
At the step 212, the content of the counter SET CNT is cleared, the CW/CCW flag is shifted to the CW position, the present position OUTPUT is increased by one (1). After this step 212, the flow proceeds to a step 215.
At the step 210, there is an interogation whether the content of the counter SET_CNT is greater than or equal to five (5) or not. If this is the case (YES), the flow proceeds to a step 214. If the interrogation at the step 214 results in negative (NO), the flow proceeds to a step 213. At the step 213, there is an interrogation whether the CW/CCW flag takes the CW state or CCW state. If the interrogation at the step 213 indicates that CW/CCW flag takes the CW position, the flow proceeds to the step 207, while if it indicates that CW/CCW flag takes the CCW position, the flow proceedsa to the step 214.
At the step 214, the content of the counter SET CNT is cleared, the CW/CCW flag is shifted to the CCW position, the present position OUTPUT is decreased by one (1). After this step 214, the flow proceeds to the step 215.
At the step 215, there is ouputted a drive signal instructing a step-up in response to increment of the present position OUTPUT or a drive signal instructing a step-down in response to decrement of the present position OUTPUT. The drive signal is supplied to the drive circuit 160 (see Fig. 2). After this step 215, the flow come to an end.
Upon receiving the step-up indicative drive signal, the drive circuit 160 causes the pulse motor 152 to turn clockwise by one step. Upon receiving the step-down indicative drive signal, the drive circuit 160 causes the pulse motor 152 to turn counterclockwise by one step.
From the previous description, it is clear that the SETTLING flag is act When it is determined that the pulse motor 152 must invert its direction of motion (see a flow along step 208, 209, 211 and 207, or a flow along step 208, 210, 213 and 207) or when the present position OUTPUT is equal to the target position TARGET (see a flow along step 205, 206 and 207). After the SETTLING flag has been set, execution of a flow along step 201, 202 and 203 is repeated until the content of the counter SET_CNT becomes equal to five (5), see steps 202 and 203. In other words, activation the pulse motor 152 is suspended for a predetermined period of time, i.e., 0.5 msec., as long as 5 cycle time. This process is called as a settlling process. The predetermined period of time is called as a settling time. The length of this settling time is determined based on the attenuation factor of the resonance inducing vibration. Upon elapse of the settling time, the the pulse motor 152 become ready to turn to reach the available target position TARGET (see a flow along step 208, 209 202 and 215 and a flow along step 208, 210, 214 and 215). It is to be noted that since the content of the counter SET_ CNT is five (5) immediately after elapse of the settling time, the interrogation at the step 211 or 213 is skipped and thus not made.
It will now be appreciasted that during the settling time, the resonance inducing vibration is attenuated and thus the pulse motor 152 starts to turn after the resonance vibration has decreased sufficiently. Thus, the loss of synchronism of the pulse motor 152 can be avoided.
Referring again to Figs. 24A, 24B, 24C and 24D, it will be recognized that owing to the settling time, the pulse motor 152 moves smoothly with any loss of synchronism.

Claims

A vehicular suspension system comprising:
a hydraulic damper including a valve element (34) having a plurality of positions and an actuator (152) drivingly coupled with the valve element (34); and
a control unit (154) operatively coupled with the actuator (152),
characterized in that the actuator (152) is held stationary for a predetermined period of time after it has been determined that the actuator (152) must invert its direction of motion to reach a target position (TARGET).
A vehicular suspension system as claimed in claim 1, characterized in that said actuator (152) is held stationary for the predetermined period of time after it has been determined that said actuator is at the target position (step 205).
A vehicular suspension system as claimed in claim 1 or 2, characterized in that after elapse of the predetermined period of time, said actuator (132) resume its motion to reach the target position.
A vehicular suspension system as claimed in claim 3, characterized in that a present position of the actuator (152) is compared with the target position to determine which direction the actuator (152) should move in.
A vehicular Suspension system as claimed in claim 4, characterized in that a flag (SETTLING) is set when it is determined that the actuator (132) must invert its direction of motion to reach the target position (TARGET) or when it is determined that the present position of said actuator is equal to the target position.
A vehicular suspension system as claimed in claim 5, characterized in that while the flag (SETTLING) is set, comparison of the present position with the target position is suspended.
A vehicular suspension system as claimed in claim 6, characterized in that the flag (SETTLING) is kept set for the predetermined period of time.
A vehicular suspension system as claimed in claim 7, characterized in that the flag (SETTLING) is cleared upon elapse of the predetermined period of time.
A vehicular suspension system as claimed in claim 8, characterized in that when the flag (SETTLING) is cleared, comparison of the present position (OUTPUT) with the target position (TARGET) is repeated at regular intervals.
A vehicular suspension system as claimed in claim 9, characterized in that the present result of the comparison and the immediately previously obtained result of the comparison are compared to determine whether the actuator (152) must invert its direction of motion.
A vehicular suspension system as claimed in claim 10, characterized in that immediately after elapse of the predetermined period of time, a result of the comparison is not campared with any previous results of the comparison.
A vehicular suspension system as claimed in claim 1, characterized in that the actuator is a pulse motor.
A method of controlling a vehicular suspension system comprising:
a hydraulic damper including a valve element (34) having a plurality of positions and an actuator (152) drivingly coupled with the valve element (34); and
a control unit (154) operatively coupled with the actuator (152),
characterized in that the actuator (152) is held stationary for a predetermined period of time after it has been determined that the actuator (152) must invert its direction of motion to reach a target position (TARGET).